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The U-2A is powered by the J57-P-37A engine produced by Pratt & Whitney and has a thrust of 10,500 pounds. In 1958, the U-2A was replaced with a J75-P-13A engine with a thrust of 15,800 pounds and upgraded to the U-2C. In 1959, in order to increase the air intake of the U-2C engine, the inlet entrance was modified and enlarged. In 1966, the U-2C was replaced with a J75-P-13B engine with a thrust of 17,000 pounds, and the inlet was modified again. In 1967, the redesigned U-2R with greater endurance and more payload began to fly. By 1968, the U-2R replaced the severely damaged U-2C and began the service life of another series of U-2 fleets.
Feature:
- Landing-gear doors can be selected position in open or closed.
- Airbrake can be selected position in open or closed.
- Accurate cockpit details.
- Appropriative"type b" camera only for u-2c.
- "Type b" camera can be displayed independently.
- Two types intake.
- Long dorsal electronics fairing.
- "Sugar scoop" infrared deflector.
- Two types decal, USAF and ROCAF 35th squadron / "black cat" squadron.